<p>A centrifugal force bearing having a means for providing a steady pitching moment is disclosed. The centrifugal force bearing may optionally comprise a coning means. A rotor system having the centrifugal force bearing is disclosed. A rotary-wing aircraft having the centrifugal force bearing is disclosed.</p>
申请公布号
WO2008048206(A2)
申请公布日期
2008.04.24
申请号
WO2006US23895
申请日期
2006.06.20
申请人
BELL HELICOPTER TEXTRON INC.;STAMPS, FRANK, B.;RAUBER, RICHARD
